View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40069U 26109.22874803 +.00000000 +00000-0 +44578-4 0 00006
2 40069 98.5078 87.0690 0005100 197.2829 162.8176 14.21443876 03
| Epoch (UTC): | 19 April 2026 05:29:23 |
| Eccentricity: | 0.0005100 |
| inclination: | 98.5078° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 87.0690° |
| argument of perigee: | 197.2829° |
| revolutions per day: | 14.21443876 |
| mean anomaly at epoch: | 162.8176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|